Investigation of Channel Interactions in Nested Hall Thruster
Investigation of Channel Interactions in Nested Hall Thruster
Combustor Dilution Hole Placement and Its Effect on the Turbine Inlet Flowfield
Combustor Dilution Hole Placement and Its Effect on the Turbine Inlet Flowfield
Introduction: Special Section on Pressure Gain Combustion
Impact of Weld Joint on Compressor Blade Performance
Impact of Weld Joint on Compressor Blade Performance
Theoretical Analysis of Dual-Thrust Rocket Motors with Intermediate Nozzle
Theoretical Analysis of Dual-Thrust Rocket Motors with Intermediate Nozzle
Numerical Analysis of Curved Thrusters for Multichamber Aerospike Engines in Flight Conditions
Numerical Analysis of Curved Thrusters for Multichamber Aerospike Engines in Flight Conditions
Rate-Controlled Constrained Equilibrium for Nozzle and Shock Flows
Rate-Controlled Constrained Equilibrium for Nozzle and Shock Flows
Combustion Dynamics in Postchamber of Hybrid Rocket Using CH Radical Chemiluminescence Images
Chemical-Equilibrium Analysis with Adjoint Derivatives for Propulsion Cycle Analysis
Chemical-Equilibrium Analysis with Adjoint Derivatives for Propulsion Cycle Analysis
Background Flow Model of Hall Thruster Neutral Ingestion
Background Flow Model of Hall Thruster Neutral Ingestion
Influences of Inlet Geometry Modification on Scramjet Flow and Combustion Dynamics
Influences of Inlet Geometry Modification on Scramjet Flow and Combustion Dynamics
Modeling Cracks in Nonlinear Viscoelastic Media Subjected to Thermal Loading
Factors Affecting the Primary Combustion Products of Boron-Based Fuel-Rich Propellants
Factors Affecting the Primary Combustion Products of Boron-Based Fuel-Rich Propellants
Chemical Nonequilibrium Modeling of Low-Power Nitrogen/Hydrogen Arcjet Thrusters
Assessment of Engine and Vehicle Performance Using Integrated Hybrid-Electric Propulsion Models
Optimization of a Rocket Nozzle Side Load Reduction Device
Optimization of a Rocket Nozzle Side Load Reduction Device
Effect of Purge Flow Swirl on Hot-Gas Ingestion into Turbine Rim Cavities
Spacecraft-Charging Characteristics Induced by the Operation of Electrospray Thrusters
Spacecraft-Charging Characteristics Induced by the Operation of Electrospray Thrusters